scholarly journals Flow Characteristics of Plane Wall Jet with Curved Walls on Both Sides

2007 ◽  
Vol 27 (Supplement2) ◽  
pp. 73-74
Author(s):  
Yuki MIHARA ◽  
Satoshi KIKUCHI ◽  
Yasuaki KOZATO ◽  
Shigeki IMAO
2006 ◽  
Vol 49 (4) ◽  
pp. 914-920 ◽  
Author(s):  
Shigeki IMAO ◽  
Satoshi KIKUCHI ◽  
Yasuaki KOZATO ◽  
Takayasu HAYASHI

2018 ◽  
Vol 35 (1) ◽  
pp. 211-234
Author(s):  
Zhitao Yan ◽  
Yongli Zhong ◽  
William E. Lin ◽  
Eric Savory ◽  
Yi You

PurposeThis paper examines various turbulence models for numerical simulation of a steady, two-dimensional (2-D) plane wall jet without co-flow using the commercial CFD software (ANSYS FLUENT 14.5). The purpose of this paper is to decide the most suitable and most economical method for steady, 2-D plane wall jet simulation.Design/methodology/approachSeven Reynolds-averaged Navier–Stokes (RANS) turbulence models were evaluated with respect to typical jet scaling parameters such as the jet half-height and the decay of maximum jet velocity, as well as coefficients from the law of the wall and for skin friction. Then, a plane wall jet generating from a rectangular slot of 1:6 aspect ratio located adjacent to the wall was investigated in a three-dimensional (3-D) model using large eddy simulation (LES) and the Stress-omega Reynolds stress model (SWRSM), with the results compared to experimental measurements.FindingsThe comparisons of these simulated flow characteristics indicated that the SWRSM was the best of the seven RANS models for simulating the turbulent wall jet. When scaled with outer variables, LES and SWRSM gave generally indistinguishable mean velocity profiles. However, SWRSM performed better for near-wall mean velocity profiles when scaled with inner variables. In general, the results show that LES performed reasonably well when predicting the Reynolds stresses.Originality/valueThe main contribution of this article is in determining the capabilities of different RANS turbulence closures and LES for the prediction of the 2-D steady wall jet flow to identify the best modelling approach.


2015 ◽  
Vol 56 (5) ◽  
Author(s):  
Ahmed Kaffel ◽  
Jean Moureh ◽  
Jean-Luc Harion ◽  
Serge Russeil

1989 ◽  
Vol 111 (1) ◽  
pp. 78-86 ◽  
Author(s):  
R. MacMullin ◽  
W. Elrod ◽  
R. Rivir

The effects of the longitudinal turbulence intensity parameter of free-stream turbulence (FST) on heat transfer were studied using the aggressive flow characteristics of a circular tangential wall jet over a constant heat flux surface. Profile measurements of velocity, temperature, integral length scale, and spectra were obtained at downstream locations (2 to 20 x/D) and turbulence intensities (7 to 18 percent). The results indicated that the Stanton number (St) and friction factor (Cf) increased with increasing turbulence intensity. The Reynolds analogy factor (2St/Cf) increased up to turbulence intensities of 12 percent, then became constant, and decreased after 15 percent. This factor was also found to be dependent on the Reynolds number (Rex) and plate configuration. The influence of length scale, as found by previous researchers, was inconclusive at the conditions tested.


Author(s):  
Iftekhar Z. Naqavi ◽  
James C. Tyacke ◽  
Paul G. Tucker

1984 ◽  
Vol 27 (224) ◽  
pp. 188-195
Author(s):  
Kazuhiro MURAI ◽  
Masao TAGA ◽  
Koji AKAGAWA

KSME Journal ◽  
1993 ◽  
Vol 7 (2) ◽  
pp. 101-112 ◽  
Author(s):  
Soon Hyun Yoon ◽  
Kyung Chun Kim ◽  
Dae Seong Kim ◽  
Myung Kyoon Chung

Author(s):  
Zifeng Yang ◽  
Anand Gopa Kumar ◽  
Hirofumi Igarashi ◽  
Hui Hu

An experimental study was conducted to quantify the flow characteristics of wall jets pertinent to trailing edge cooling of turbine blades. A high-resolution stereoscopic PIV system was used to conduct detailed flow field measurements to quantitatively visualize the evolution of the unsteady vortex and turbulent flow structures in cooling wall jet streams and to quantify the dynamic mixing process between the cooling wall jet streams and the main stream flows. The detailed flow field measurements are correlated with the adiabatic cooling effectiveness maps measured by using pressure sensitive paint (PSP) technique to elucidate underlying physics in order to improve cooling effectiveness to protect the critical portions of turbine blades from the harsh ambient conditions.


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